If the circular orbit of a synchronous satellite is 6r above the Earth's radius r, the radius of the Earth will be the orbit of another artificial satellite at 2.5r above the Earth's surface.
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For geostationary satellite : r1=R+6R=7R T1=24 h
For second satellite : r2=R+2.5R=3.5R
Time period of satellite : T=2πGMr3 where, r is the radius of orbit
⟹ T1T2=r13r23
∴ 24T2=(7R)3(3.5R)3=221
⟹ T2=2224=62 h
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